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Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology | 論文
- Experimental Approach to Improve Ion Thruster Performance: Part 1 Effects of the Propellant Delivery Method
- Basic mechanical properties of balloon-type TEEK-L polyimide-foam and TEEK-L filled aramid-honeycomb core materials for sandwich structures
- Multi-Objective Trajectory Optimization by a Hierarchical Gradient Algorithm with Fuzzy Decision Logic : Application to Slew Maneuver Problems of a Flexible Space Structure
- Guided Modes of Electron Wave in a Si-Quantum Wire
- CURRENT STATUS OF ROCKET DEVELOPMENTS IN UNIVERSITIES : DEVELOPMENT OF A SMALL HYBRID ROCKET WITH A SWIRLING OXIDIZER FLOW TYPE ENGINE
- Feasibility Study on C 60 Plasma Application to Ion Thruster
- Enhancement by Ascorbic Acid 2-Glucoside or Repeated Additions of Ascorbate of Mitogen-Induced IgM and IgG Productions by Human Peripheral Blood Lymphocytes.